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1. 发明申请

US20150232174A1 HUB-MOUNTED ACTIVE VIBRATION CONTROL (HAVC) DEVICES, SYSTEMS, AND METHODS 审中-公开
标题翻译： HUB安装的主动振动控制（HAVC）设备，系统和方法
公开(公告)号：US20150232174A1
公开(公告)日：2015-08-20
申请号：US14434781
申请日：2013-10-23
申请人： Mark R. JOLLY , Russell E. ALTIERI , Wayne L. WINZENZ , Warren F. BRANNAN , Paul R. BLACK , Doug A. SWANSON , LORD CORPORATION
发明人： Mark R. Jolly , Russell E. Altieri , Wayne L. Winzenz , Warren F. Brannan , Paul R. Black , Doug A. Swanson
IPC分类号： B64C27/00 , F16F15/18 , F16F15/14
CPC分类号： B64C27/001 , B64C2027/003 , B64C2027/004 , F16F15/1485 , F16F15/18 , Y10T74/2128
摘要： Hub-mounted active vibration control (HAVC) devices, systems, and related methods are provided. An HAVC device (100) includes a housing (206) having a tolerance ring (600) attached to a rotary hub (702). The tolerance ring can accommodate dissimilar coefficients of thermal expansion between dissimilar metals. The HAVC device can also include a plurality of coaxial ring motors (308A, 308B, 310A, 310B) configured to rotate a plurality of imbalance masses for controlling vibration. An HAVC system can further include a de-icing distributor (208) for communicating instructions to one or more heating sources (HS) provided at one or more rotary blades (802) of a vehicle or aircraft. A method of controlling vibratory loads occurring at a moving platform can include providing a moving platform, mounting a vibration control device to a portion of the moving platform, and rotating at least one pair of imbalance masses such that the combined forces of the masses substantially cancel unwanted vibration of the platform.
摘要翻译：提供了集线器安装的主动振动控制（HAVC）设备，系统和相关方法。 HAVC装置（100）包括具有附接到旋转毂（702）的公差环（600）的壳体（206）。公差环可以适应不同金属之间的不同的热膨胀系数。 HAVC装置还可以包括多个同轴环电动机（308A，308B，310A，310B），其被配置为旋转多个不平衡块以控制振动。 HAVC系统还可以包括用于将指令传送到设置在车辆或飞行器的一个或多个旋转叶片（802）处的一个或多个加热源（HS）的除冰分配器（208）。一种控制在移动平台上发生的振动荷载的方法可以包括提供移动平台，将振动控制装置安装到移动平台的一部分，以及旋转至少一对不平衡块，使得组合力基本上消除平台不必要的振动。

2. 发明申请

US20150303633A1 IMPROVED SLIP RING DEVICES, SYSTEMS, AND METHODS 审中-公开
标题翻译：改进的滑环设备，系统和方法
公开(公告)号：US20150303633A1
公开(公告)日：2015-10-22
申请号：US14441003
申请日：2013-11-08
申请人： Russell Altieri , Mark R. Jolly , Warren F. Brannan , Donald R. Morris, JR. , Michael W. Trull , Richard Martin , LORD Corporation
发明人： Russell E. Altieri , Mark R. Jolly , Warren F. Brannan , Donald R. Morris, JR. , Michael W. Trull , Richard Martin
IPC分类号： H01R39/08 , H02J5/00 , H04B5/00 , G01R31/04 , G01R31/327
CPC分类号： H01R39/08 , B64C27/32 , B64D15/12 , G01R31/04 , G01R31/327 , H01R39/24 , H04B5/0037
摘要： Improvements to slip rings (200) and methods for the operation thereof include an improved slip ring assembly (200) that has a stationary element (202), a rotating element (210) rotatable with respect to the stationary (202) element, a bearing assembly coupled between the stationary element (202) and the rotating element (210), and one or more contact brushes (213) on one of the stationary element (202) or the rotating element (210). In some embodiments, the bearing assembly includes a primary bearing, a secondary bearing, a shear pin coupling the secondary bearing to the primary bearing, and an electrical monitoring circuit (206) in communication with the shear pin. In some embodiments, the one or more contact brushes (213) includes one or more metal fiber brushes constructed of a plurality of metal fibers that are configured to transmit one or more of electrical power or data between the stationary element (202) and the rotating element (210).
摘要翻译：滑环（200）的改进及其操作方法包括改进的滑环组件（200），其具有静止元件（202），相对于静止（202）元件可旋转的旋转元件（210），轴承联接在固定元件（202）和旋转元件（210）之间的组件，以及在固定元件（202）或旋转元件（210）之一上的一个或多个接触刷（213）。在一些实施例中，轴承组件包括主轴承，次轴承，将次轴承连接到主轴承的剪切销以及与剪切销连通的电监控回路（206）。在一些实施例中，一个或多个接触刷（213）包括由多个金属纤维构成的一个或多个金属纤维刷，所述多个金属纤维构造成在固定元件（202）和旋转的（202）之间传递电力或数据中的一个或多个元件（210）。

3. 发明授权

US08162606B2 Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations 有权
标题翻译：直升机轮毂安装的振动控制和圆形力产生系统，用于消除振动
公开(公告)号：US08162606B2
公开(公告)日：2012-04-24
申请号：US12419775
申请日：2009-04-07
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： F04D29/26 , F01D5/26 , B64C11/00
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
摘要： A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration control system rotating with the rotating rotary wing hub. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, and a distributed force generation data communications network link.
摘要翻译：一种包括车辆振动控制系统的旋翼飞机。车辆振动控制系统包括旋转轮毂安装的振动控制系统，旋转轮毂安装的振动控制系统安装到旋转的旋翼轮毂上，旋转轮毂安装的振动控制系统与旋转的旋翼轮毂一起旋转。车辆振动控制系统包括旋转翼飞行器构件传感器，用于输出与旋转的旋翼轮毂构件相对于非旋转体相对旋转相关的旋转翼飞行器构件数据，至少第一非旋转体振动传感器，至少第一非旋转体振动传感器，至少输出与振动相关的第一非旋转体振动传感器数据，至少第一非旋转体圆周力产生器，与所述非旋转体固定连接的所述至少第一非旋转体圆周力产生器，以及分布力产生数据通信网络链接。

4. 发明授权

US07925392B2 Aircraft vehicular propulsion system monitoring device and method 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US07925392B2
公开(公告)日：2011-04-12
申请号：US12099461
申请日：2008-04-08
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
IPC分类号： G01B7/24 , G01L3/00 , G06F15/00
CPC分类号： B64C29/005 , B64F5/60 , G01B7/31
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vertical propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The collar misalignment measuring system of the invention provide a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴轴和联轴器的方法和系统。测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机，其中垂直推进动态旋转驱动轴系统和联轴器被实时监控。车轴联轴器未对准测量系统利用多个位置传感器来提供对推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。传感器的相对位置通过结构框架从旋转目标的外部刚性固定。本发明的套环未对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量，其涉及在飞行器车辆的操作中的旋转轴联轴器的关键性能。该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。

5. 发明授权

US06954685B2 Aircraft vehicular propulsion system monitoring device and method 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US06954685B2
公开(公告)日：2005-10-11
申请号：US10421325
申请日：2003-04-23
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
IPC分类号： B64C29/00 , B64D45/00 , B64F5/00 , G01B7/31 , G01M13/02
CPC分类号： G01B7/31 , B64C29/005 , B64F5/60
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vertical propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The collar misalignment measuring system of the invention provide a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴轴和联轴器的方法和系统。测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机，其中垂直推进动态旋转驱动轴系统和联轴器被实时监控。车轴联轴器未对准测量系统利用多个位置传感器来提供对推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。传感器的相对位置通过结构框架从旋转目标的外部刚性固定。本发明的套环未对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量，其涉及在飞行器车辆的操作中的旋转轴联轴器的关键性能。该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。

6. 发明授权

US08639399B2 Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations 有权
标题翻译：具有抑制振动的分布式主动振动控制系统和旋翼飞机
公开(公告)号：US08639399B2
公开(公告)日：2014-01-28
申请号：US13333196
申请日：2011-12-21
申请人： Mark R. Jolly , Askari Badre-Alam , Russell E. Altieri , Andrew D. Meyers
发明人： Mark R. Jolly , Askari Badre-Alam , Russell E. Altieri , Andrew D. Meyers
IPC分类号： G05D1/00
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： A method and system is disclosed for controlling problematic vibrations in an aircraft having. The method and system have the ability to cancel problematic rotary wing helicopter vibrations using independent active force generator power and with distributed communications therebetween.
摘要翻译：公开了一种用于控制飞机中有问题的振动的方法和系统。该方法和系统具有使用独立的主动力发生器功率并且在其间具有分布式通信来消除有问题的旋转翼直升机振动的能力。

7. 发明申请

US20120136533A1 HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEMS FOR CANCELING VIBRATIONS 有权
标题翻译：直升机振动控制系统和消除振动的循环发电系统
公开(公告)号：US20120136533A1
公开(公告)日：2012-05-31
申请号：US12971026
申请日：2010-12-17
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： G06F19/00 , G05D15/00 , B64C27/473 , G05D19/00 , F16F7/00 , F16F7/10
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
摘要： A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, the at least first nonrotating body circular force generator controlled to produce a rotating force with a controllable rotating force magnitude and a controllable rotating force phase, the controllable rotating force magnitude controlled from a minimal force magnitude up to a maximum force magnitude, and with the controllable rotating force phase controlled in reference to the rotary wing aircraft member sensor data correlating to the relative rotation of the rotating rotary wing hub rotating relative to the nonrotating body wherein the vibration sensed by the at least first nonrotating body vibration sensor is reduced.
摘要翻译：一种包括车辆振动控制系统的旋翼飞机。车辆振动控制系统包括旋转翼飞行器构件传感器，用于输出与旋转的旋翼轮毂构件相对于非旋转体相对旋转相关的旋转翼飞行器构件数据，至少第一非旋转体振动传感器，至少至少第一非旋转体圆周力产生器，至少第一非旋转体圆周力产生器，其与所述非旋转体固定连接，所述至少第一非旋转体振动传感器，至少第一非旋转体振动传感器，至少第一非旋转体振动传感器，主体圆形力发生器被控制以产生具有可控旋转力量级和可控旋转力相位的旋转力，可控旋转力量值从最小力量控制到最大力量值，并且可控旋转力相位被控制在参考旋转翼型飞行器构件传感器数据与旋转的旋转翼型轮毂相对于非旋转体相对旋转，其中由至少第一非旋转体振动传感器感测的振动减小。

8. 发明申请

US20090055129A1 AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US20090055129A1
公开(公告)日：2009-02-26
申请号：US12099461
申请日：2008-04-08
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
IPC分类号： G01B7/24 , G06F15/00
CPC分类号： B64C29/005 , B64F5/60 , G01B7/31
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vertical propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The collar misalignment measuring system of the invention provide a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴轴和联轴器的方法和系统。测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机，其中垂直推进动态旋转驱动轴系统和联轴器被实时监控。车轴联轴器未对准测量系统利用多个位置传感器来提供对推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。传感器的相对位置通过结构框架从旋转目标的外部刚性固定。本发明的套环未对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量，其涉及在飞行器车辆的操作中的旋转轴联轴器的关键性能。该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。

9. 发明授权

US09073627B2 Helicopter vibration control system and circular force generation systems for canceling vibrations 有权
标题翻译：直升机振动控制系统和用于消除振动的圆形力产生系统
公开(公告)号：US09073627B2
公开(公告)日：2015-07-07
申请号：US12971026
申请日：2010-12-17
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： G06F19/00 , G05D15/00 , G05D19/00 , B64C27/00 , F16F15/22
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
摘要： A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, the at least first nonrotating body circular force generator controlled to produce a rotating force with a controllable rotating force magnitude and a controllable rotating force phase, the controllable rotating force magnitude controlled from a minimal force magnitude up to a maximum force magnitude, and with the controllable rotating force phase controlled in reference to the rotary wing aircraft member sensor data correlating to the relative rotation of the rotating rotary wing hub rotating relative to the nonrotating body wherein the vibration sensed by the at least first nonrotating body vibration sensor is reduced.
摘要翻译：一种包括车辆振动控制系统的旋翼飞机。车辆振动控制系统包括旋转翼飞行器构件传感器，用于输出与旋转的旋翼轮毂构件相对于非旋转体相对旋转相关的旋转翼飞行器构件数据，至少第一非旋转体振动传感器，至少至少第一非旋转体圆周力产生器，至少第一非旋转体圆周力产生器，其与所述非旋转体固定连接，所述至少第一非旋转体振动传感器，至少第一非旋转体振动传感器，至少第一非旋转体振动传感器，主体圆形力发生器被控制以产生具有可控旋转力量级和可控旋转力相位的旋转力，可控旋转力量值从最小力量控制到最大力量值，并且可控旋转力相位被控制在参考旋转翼型飞行器构件传感器数据与旋转的旋转翼型轮毂相对于非旋转体相对旋转，其中由至少第一非旋转体振动传感器感测的振动减小。

10. 发明授权

US08090482B2 Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations 有权
标题翻译：具有抑制振动的分布式主动振动控制系统和旋翼飞机
公开(公告)号：US08090482B2
公开(公告)日：2012-01-03
申请号：US12288867
申请日：2008-10-24
申请人： Mark R. Jolly , Askari Badre-Alam , Russell E. Altieri , Andrew D. Meyers
发明人： Mark R. Jolly , Askari Badre-Alam , Russell E. Altieri , Andrew D. Meyers
IPC分类号： G05D1/00
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： An aircraft with an aerostructure and at least one rotating machine creating troublesome vibrations, with the aircraft including a power source outputting electromagnetic force generator power outputs, a first and second distributed active vibration electromagnetic force generator, the first and second force generator including a distributed electronic control system and an electromagnetically driven mass, the force generators fixed to the aerostructure at first and second distributed active vibration control system sites, and electrical power distribution lines connecting the force generators with the power source with the power outputs outputted to the electromagnetic force generators, and a distributed force generator data communications network linking together the first and second distributed electronic control systems wherein the distributed electronic control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.
摘要翻译：具有航空结构的飞机和至少一个旋转机器产生麻烦的振动，飞机包括输出电磁力发生器功率输出的电源，第一和第二分布式主动振动电磁力发生器，第一和第二力发生器包括分布式电子控制系统和电磁驱动质量块，将力发生器固定在第一和第二分布式主动振动控制系统位置处的航空结构，以及将力发生器与电源连接的电力分配线与输出到电磁力发生器的功率输出，以及将第一和第二分布式电子控制系统连接在一起的分布式力发生器数据通信网络，其中分布式电子控制系统通过分布式力发生器数据通信传递力发生器振动控制数据独立于电力配电线路以最小化麻烦的振动。

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